The present work is concerned with predicting the unsteady flow considered to be the cause of the structural failure of twin vertical tail aircraft. An engineering tool has been produced for high angle of attack aerodynamics using the simplest physical models. The main innovation behind this work is its emphasis on the modeling of two key aspects of the dominant physics associated with high angle-of-attack airflows, namely unsteady separation and vortex breakdown.


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    Titel :

    Development of an engineering level prediction method for high angle of attack aerodynamics


    Beteiligte:

    Kongress:

    AIAA, Aerospace Sciences Meeting and Exhibit ; 1993 ; Reno, NV, United States


    Erscheinungsdatum :

    01.01.1993


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Development of an engineering level prediction method for high angleof attack aerodynamics

    REISENTHEL, PATRICK / RODMAN, LAURA / NIXON, DAVID | AIAA | 1993


    High Angle of Attack Aerodynamics

    Champigny, P. / AGARD; Fluid Dynamics Panel | British Library Conference Proceedings | 1994


    High Angle of Attack - Aerodynamics

    John E. Lamar | NTRS | 1992


    High Angle of Attack Aerodynamics

    P. Champigny | NTIS | 1994